WO1997011311A3 - Brenner, insbesondere für eine gasturbine - Google Patents

Brenner, insbesondere für eine gasturbine Download PDF

Info

Publication number
WO1997011311A3
WO1997011311A3 PCT/DE1996/001756 DE9601756W WO9711311A3 WO 1997011311 A3 WO1997011311 A3 WO 1997011311A3 DE 9601756 W DE9601756 W DE 9601756W WO 9711311 A3 WO9711311 A3 WO 9711311A3
Authority
WO
WIPO (PCT)
Prior art keywords
burner
current
annular gap
gas turbine
arrangement
Prior art date
Application number
PCT/DE1996/001756
Other languages
English (en)
French (fr)
Other versions
WO1997011311A2 (de
Inventor
Bernd Prade
Bernhard Schetter
Holger Streb
Original Assignee
Siemens Ag
Bernd Prade
Bernhard Schetter
Holger Streb
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Siemens Ag, Bernd Prade, Bernhard Schetter, Holger Streb filed Critical Siemens Ag
Priority to DE59608389T priority Critical patent/DE59608389D1/de
Priority to EP96942244A priority patent/EP0851990B1/de
Priority to JP51231697A priority patent/JP3939756B2/ja
Publication of WO1997011311A2 publication Critical patent/WO1997011311A2/de
Publication of WO1997011311A3 publication Critical patent/WO1997011311A3/de
Priority to US09/047,164 priority patent/US6038864A/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/20—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone
    • F23D14/22—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other
    • F23D14/24—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other at least one of the fluids being submitted to a swirling motion
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C7/00—Combustion apparatus characterised by arrangements for air supply
    • F23C7/002—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion
    • F23C7/004—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion using vanes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/26—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid with provision for a retention flame

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)
  • Gas Burners (AREA)

Abstract

Die Erfindung betrifft einen Brenner mit einer Achse (1) und einer bezüglich dieser rotationssymmetrischen Anordnung aus einem Außenmantel (2) und einem dazu koaxialen Innenmantel (3). Diese definiert einen von einem Eintritt (5) zu einem Austritt (6) reichenden Ringspalt (4) zur Führung eines Stromes (7) eines Sauerstoff enthaltenden Gases. In dem Ringspalt (4) angeordnet ist eine Vielzahl von Düsen (9) zur Zuführung eines Brennstoffes zu dem Strom (7) sowie ein Drallgitter (8). Die Anordnung aus dem Außenmantel (2) und dem Innenmantel (3) ist derart gestaltet, daß der Strom (7) den Ringspalt (4) zwischen dem Drallgitter (8) und dem Austritt (6) mit einer im wesentlichen konstanten meridionalen Geschwindigkeit durchfließt. Der Brenner ist besonders geeignet zur Verwendung in einer Gasturbine (15, 16, 17).
PCT/DE1996/001756 1995-09-22 1996-09-17 Brenner, insbesondere für eine gasturbine WO1997011311A2 (de)

Priority Applications (4)

Application Number Priority Date Filing Date Title
DE59608389T DE59608389D1 (de) 1995-09-22 1996-09-17 Brenner, insbesondere für eine gasturbine
EP96942244A EP0851990B1 (de) 1995-09-22 1996-09-17 Brenner, insbesondere für eine gasturbine
JP51231697A JP3939756B2 (ja) 1995-09-22 1996-09-17 特にガスタービン用のバーナ
US09/047,164 US6038864A (en) 1995-09-22 1998-03-23 Burner with annular gap and gas flow with constant meridional velocity through the annular gap and gas turbine having the burner

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19535287.4 1995-09-22
DE19535287 1995-09-22

Related Child Applications (1)

Application Number Title Priority Date Filing Date
US09/047,164 Continuation US6038864A (en) 1995-09-22 1998-03-23 Burner with annular gap and gas flow with constant meridional velocity through the annular gap and gas turbine having the burner

Publications (2)

Publication Number Publication Date
WO1997011311A2 WO1997011311A2 (de) 1997-03-27
WO1997011311A3 true WO1997011311A3 (de) 1997-05-15

Family

ID=7772905

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/DE1996/001756 WO1997011311A2 (de) 1995-09-22 1996-09-17 Brenner, insbesondere für eine gasturbine

Country Status (7)

Country Link
US (1) US6038864A (de)
EP (1) EP0851990B1 (de)
JP (1) JP3939756B2 (de)
DE (1) DE59608389D1 (de)
ES (1) ES2169273T3 (de)
RU (1) RU2156405C2 (de)
WO (1) WO1997011311A2 (de)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4130475B2 (ja) * 1996-09-09 2008-08-06 シーメンス アクチエンゲゼルシヤフト 空気内で燃料を燃焼する装置とその方法
EP0995066B1 (de) * 1997-07-17 2001-09-26 Siemens Aktiengesellschaft Brenneranordnung für eine feuerungsanlage, insbesondere eine gasturbinenbrennkammer
US6161387A (en) * 1998-10-30 2000-12-19 United Technologies Corporation Multishear fuel injector
DE10104695B4 (de) * 2001-02-02 2014-11-20 Alstom Technology Ltd. Vormischbrenner für eine Gasturbine
US6551098B2 (en) * 2001-02-22 2003-04-22 Rheem Manufacturing Company Variable firing rate fuel burner
US6539721B2 (en) 2001-07-10 2003-04-01 Pratt & Whitney Canada Corp. Gas-liquid premixer
US6698208B2 (en) * 2001-12-14 2004-03-02 Elliott Energy Systems, Inc. Atomizer for a combustor
US6786047B2 (en) 2002-09-17 2004-09-07 Siemens Westinghouse Power Corporation Flashback resistant pre-mix burner for a gas turbine combustor
US6848260B2 (en) 2002-09-23 2005-02-01 Siemens Westinghouse Power Corporation Premixed pilot burner for a combustion turbine engine
EP1645805A1 (de) * 2004-10-11 2006-04-12 Siemens Aktiengesellschaft Brenner für fluidische Brennstoffe und Verfahren zum Betreiben eines derartigen Brenners
US7370466B2 (en) * 2004-11-09 2008-05-13 Siemens Power Generation, Inc. Extended flashback annulus in a gas turbine combustor
EP1944547A1 (de) * 2007-01-15 2008-07-16 Siemens Aktiengesellschaft Steuerverfahren zur Kraftstoffspaltung
US20080276622A1 (en) * 2007-05-07 2008-11-13 Thomas Edward Johnson Fuel nozzle and method of fabricating the same
US8113000B2 (en) * 2008-09-15 2012-02-14 Siemens Energy, Inc. Flashback resistant pre-mixer assembly
EP2312215A1 (de) 2008-10-01 2011-04-20 Siemens Aktiengesellschaft Brenner und Verfahren zum Betrieb eines Brenners
EP2236934A1 (de) 2009-03-18 2010-10-06 Siemens Aktiengesellschaft Brenneranordnung
EP2264370B1 (de) * 2009-06-16 2012-10-10 Siemens Aktiengesellschaft Brenneranordnung für eine Verfeuerungsanlage zum Verfeuern fluidischer Brennstoffe und Verfahren zum Betrieb einer solchen Brenneranordnung
US8387393B2 (en) * 2009-06-23 2013-03-05 Siemens Energy, Inc. Flashback resistant fuel injection system
WO2012118397A1 (ru) * 2011-02-28 2012-09-07 Открытое Акционерное Общество "Силовые Машины - Зтл, Лмз, Электросила, Энергомашэкспорт" (Оао "Силовые Машины") Горелка
US9046262B2 (en) * 2011-06-27 2015-06-02 General Electric Company Premixer fuel nozzle for gas turbine engine
WO2019020350A1 (de) 2017-07-27 2019-01-31 Siemens Aktiengesellschaft Gasturbinenbrenner mit vorgemischten strahlflammen

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0193838A2 (de) * 1985-03-04 1986-09-10 Siemens Aktiengesellschaft Brenneranordnung für Feuerungsanlagen, insbesondere für Brennkammern von Gasturbinenanlagen sowie Verfahren zu ihrem Betrieb
WO1992019913A1 (de) * 1991-04-25 1992-11-12 Siemens Aktiengesellschaft Brenneranordnung, insbesondere für gasturbinen, zur schadstoffarmen verbrennung von kohlegas und anderen brennstoffen
EP0589520A1 (de) * 1992-09-24 1994-03-30 NUOVOPIGNONE INDUSTRIE MECCANICHE E FONDERIA S.p.A. Verbrennungsanlage mit niedriger Schadstoffemission für Gasturbinen
WO1995002789A1 (en) * 1993-07-16 1995-01-26 Radian Corporation APPARATUS AND METHOD FOR REDUCING NOx, CO AND HYDROCARBON EMISSIONS WHEN BURNING GASEOUS FUELS
WO1995004244A1 (en) * 1993-07-29 1995-02-09 United Technologies Corporation Fuel injector and method of operating the fuel injector

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US33896A (en) * 1861-12-10 Improved automatic
US3589127A (en) * 1969-02-04 1971-06-29 Gen Electric Combustion apparatus
US4013377A (en) * 1975-10-08 1977-03-22 Westinghouse Electric Corporation Intermediate transition annulus for a two shaft gas turbine engine
US4365753A (en) * 1980-08-22 1982-12-28 Parker-Hannifin Corporation Boundary layer prefilmer airblast nozzle
EP0276696B1 (de) * 1987-01-26 1990-09-12 Siemens Aktiengesellschaft Hybridbrenner für Vormischbetrieb mit Gas und/oder Öl, insbesondere für Gasturbinenanlagen
US4801261A (en) * 1987-03-19 1989-01-31 Eagleair, Inc. Apparatus and method for delivery of combustion air in multiple zones
DE3819899C1 (en) * 1988-06-11 1989-11-30 Daimler-Benz Aktiengesellschaft, 7000 Stuttgart, De Apparatus for generating a homogeneous mixture from a first and second medium
EP0393484B1 (de) * 1989-04-20 1992-11-04 Asea Brown Boveri Ag Brennkammeranordnung
EP0444517B1 (de) * 1990-02-26 1995-05-10 Nippondenso Co., Ltd. Selbstdiagnoseapparat in einem System zur Verhinderung des Entweichens von verdampftem Brennstoffgas
US5165241A (en) * 1991-02-22 1992-11-24 General Electric Company Air fuel mixer for gas turbine combustor
US5259184A (en) * 1992-03-30 1993-11-09 General Electric Company Dry low NOx single stage dual mode combustor construction for a gas turbine
US5323604A (en) * 1992-11-16 1994-06-28 General Electric Company Triple annular combustor for gas turbine engine
US5351477A (en) * 1993-12-21 1994-10-04 General Electric Company Dual fuel mixer for gas turbine combustor
DE4417769A1 (de) * 1994-05-20 1995-11-23 Abb Research Ltd Verfahren zum Betrieb eines Vormischbrenners
US5865609A (en) * 1996-12-20 1999-02-02 United Technologies Corporation Method of combustion with low acoustics

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0193838A2 (de) * 1985-03-04 1986-09-10 Siemens Aktiengesellschaft Brenneranordnung für Feuerungsanlagen, insbesondere für Brennkammern von Gasturbinenanlagen sowie Verfahren zu ihrem Betrieb
WO1992019913A1 (de) * 1991-04-25 1992-11-12 Siemens Aktiengesellschaft Brenneranordnung, insbesondere für gasturbinen, zur schadstoffarmen verbrennung von kohlegas und anderen brennstoffen
EP0589520A1 (de) * 1992-09-24 1994-03-30 NUOVOPIGNONE INDUSTRIE MECCANICHE E FONDERIA S.p.A. Verbrennungsanlage mit niedriger Schadstoffemission für Gasturbinen
WO1995002789A1 (en) * 1993-07-16 1995-01-26 Radian Corporation APPARATUS AND METHOD FOR REDUCING NOx, CO AND HYDROCARBON EMISSIONS WHEN BURNING GASEOUS FUELS
WO1995004244A1 (en) * 1993-07-29 1995-02-09 United Technologies Corporation Fuel injector and method of operating the fuel injector

Also Published As

Publication number Publication date
RU2156405C2 (ru) 2000-09-20
ES2169273T3 (es) 2002-07-01
EP0851990A2 (de) 1998-07-08
WO1997011311A2 (de) 1997-03-27
US6038864A (en) 2000-03-21
DE59608389D1 (de) 2002-01-17
JP3939756B2 (ja) 2007-07-04
JP2000512723A (ja) 2000-09-26
EP0851990B1 (de) 2001-12-05

Similar Documents

Publication Publication Date Title
WO1997011311A3 (de) Brenner, insbesondere für eine gasturbine
EP2128388B1 (de) Diffusor
US5579645A (en) Radially mounted air blast fuel injector
EP0349635B1 (de) Gasturbinenbrennkammer mit tangentialer brennstoffeinspritzung und zusätzlichen treibstrahlen
US7753677B2 (en) Burner
CN109595080A (zh) 操作燃烧***的方法和包括燃烧***的燃气涡轮发动机
KR960001441A (ko) 터어빈의 확산동작모드와 예비혼합동작모드 사이에서 연료를 단계화시키는 방법
EP0735318A3 (de) Kraftstoff-Einspritzdüse mit verstellbarer Geometrie
CN101949540A (zh) 对涡轮燃烧器燃料喷嘴中火焰稳定和回火的主动控制
EP1288576A3 (de) Gasturbinenbrennkammer
EP0242023A3 (de) Plasmabogenbrenner mit gasgekühlter Löschelektrode
CA2340107A1 (en) Gas turbine and gas turbine combustor
EP0870989A3 (de) Kraftstoffeinspritzanordnung für eine Gasturbinenbrennkammer
JPS63194114A (ja) ガス及び／又は油による予混合運転のための複合バーナ
US4713938A (en) Gas turbine engine gaseous fuel injector
EP1201995A3 (de) Gasturbinenverbrennungsanlage
EP0539580B1 (de) Gasturbinenbrennkammer für sehr grosse höhen
HU9400367D0 (en) Fuel atomizer
CN110006068A (zh) 用于燃气涡轮发动机燃烧器的燃料喷嘴
RU98107628A (ru) Горелка, в частности для газовой турбины
TW353135B (en) Gas pilot with radially displaced, high momentum fuel outlet, and method thereof
DE59300530D1 (de) Zylindrisches Brennkammergehäuse einer Gasturbine.
WO1998011383A3 (de) Vorrichtung und verfahren zur verbrennung eines brennstoffs in luft
US4261517A (en) Atomizing air metering nozzle
US6038863A (en) Burner arrangement for a gas turbine for preventing the ingress of fluids into a fuel passage

Legal Events

Date Code Title Description
AK Designated states

Kind code of ref document: A2

Designated state(s): CN CZ JP KR RU UA US

AL Designated countries for regional patents

Kind code of ref document: A2

Designated state(s): AT BE CH DE DK ES FI FR GB GR IE IT LU MC NL PT SE

AK Designated states

Kind code of ref document: A3

Designated state(s): CN CZ JP KR RU UA US

AL Designated countries for regional patents

Kind code of ref document: A3

Designated state(s): AT BE CH DE DK ES FI FR GB GR IE IT LU MC NL PT SE

DFPE Request for preliminary examination filed prior to expiration of 19th month from priority date (pct application filed before 20040101)
121 Ep: the epo has been informed by wipo that ep was designated in this application
WWE Wipo information: entry into national phase

Ref document number: 1996942244

Country of ref document: EP

ENP Entry into the national phase

Ref country code: JP

Ref document number: 1997 512316

Kind code of ref document: A

Format of ref document f/p: F

WWE Wipo information: entry into national phase

Ref document number: 09047164

Country of ref document: US

WWP Wipo information: published in national office

Ref document number: 1996942244

Country of ref document: EP

WWG Wipo information: grant in national office

Ref document number: 1996942244

Country of ref document: EP